View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 20203U 26146.09832720 +.00000000 +00000-0 +00000-0 0 00000
2 20203 14.7107 4.2444 0011963 18.7937 334.3468 0.99116323 07
| Epoch (UTC): | 26 May 2026 02:21:35 |
| Eccentricity: | 0.0011963 |
| inclination: | 14.7107° |
| perigee height: | 36063 km |
| apogee height: | 36164 km |
| right ascension of ascending node: | 4.2444° |
| argument of perigee: | 18.7937° |
| revolutions per day: | 0.99116323 |
| mean anomaly at epoch: | 334.3468° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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